EP3532213B1 - Apparatus and method for making thick gauge aluminum alloy articles - Google Patents
Apparatus and method for making thick gauge aluminum alloy articles Download PDFInfo
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- EP3532213B1 EP3532213B1 EP17791201.1A EP17791201A EP3532213B1 EP 3532213 B1 EP3532213 B1 EP 3532213B1 EP 17791201 A EP17791201 A EP 17791201A EP 3532213 B1 EP3532213 B1 EP 3532213B1
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- aluminum alloy
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- 229910000838 Al alloy Inorganic materials 0.000 title claims description 260
- 238000000034 method Methods 0.000 title claims description 30
- 238000005096 rolling process Methods 0.000 claims description 64
- 238000005266 casting Methods 0.000 claims description 40
- 238000010791 quenching Methods 0.000 claims description 39
- 230000000171 quenching effect Effects 0.000 claims description 35
- 238000003303 reheating Methods 0.000 claims description 24
- 238000009749 continuous casting Methods 0.000 claims description 16
- 229910052751 metal Inorganic materials 0.000 claims description 16
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- 238000011144 upstream manufacturing Methods 0.000 claims description 5
- 239000000956 alloy Substances 0.000 description 26
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- 238000005098 hot rolling Methods 0.000 description 22
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- 238000001953 recrystallisation Methods 0.000 description 7
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 229910052725 zinc Inorganic materials 0.000 description 4
- 239000011701 zinc Substances 0.000 description 4
- 238000005275 alloying Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 238000010008 shearing Methods 0.000 description 3
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Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B13/00—Metal-rolling stands, i.e. an assembly composed of a stand frame, rolls, and accessories
- B21B13/22—Metal-rolling stands, i.e. an assembly composed of a stand frame, rolls, and accessories for rolling metal immediately subsequent to continuous casting, i.e. in-line rolling of steel
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
- B21B1/22—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling plates, strips, bands or sheets of indefinite length
- B21B1/24—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling plates, strips, bands or sheets of indefinite length in a continuous or semi-continuous process
- B21B1/26—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling plates, strips, bands or sheets of indefinite length in a continuous or semi-continuous process by hot-rolling, e.g. Steckel hot mill
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
- B21B1/46—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling metal immediately subsequent to continuous casting
- B21B1/463—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling metal immediately subsequent to continuous casting in a continuous process, i.e. the cast not being cut before rolling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B15/00—Arrangements for performing additional metal-working operations specially combined with or arranged in, or specially adapted for use in connection with, metal-rolling mills
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/001—Continuous casting of metals, i.e. casting in indefinite lengths of specific alloys
- B22D11/003—Aluminium alloys
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
- B22D11/0605—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars formed by two belts, e.g. Hazelett-process
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
- B22D11/0631—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars formed by a travelling straight surface, e.g. through-like moulds, a belt
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/12—Accessories for subsequent treating or working cast stock in situ
- B22D11/1206—Accessories for subsequent treating or working cast stock in situ for plastic shaping of strands
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/12—Accessories for subsequent treating or working cast stock in situ
- B22D11/126—Accessories for subsequent treating or working cast stock in situ for cutting
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/047—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with magnesium as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
- B21B1/22—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling plates, strips, bands or sheets of indefinite length
- B21B2001/225—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling plates, strips, bands or sheets of indefinite length by hot-rolling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B3/00—Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals
- B21B2003/001—Aluminium or its alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B15/00—Arrangements for performing additional metal-working operations specially combined with or arranged in, or specially adapted for use in connection with, metal-rolling mills
- B21B2015/0057—Coiling the rolled product
Definitions
- the present disclosure relates to metallurgy generally and more specifically to metal plate manufacturing.
- US 2003/0150587 A1 is directed to a process for producing an aluminum sheet product having a controlled recrystallization using a continuous caster to cast a molten aluminum alloy into a slab comprising (a) providing a source of molten aluminum alloy, (b) providing a caster for continuously casting said molten aluminum alloy into a slab, (c) rolling said slab into a sheet product, (d) continuously annealing said sheet product at a temperature in a controlled temperature range, (e) measuring degree of recrystallization of said sheet product on a continuous basis to provide a recrystallization related signal, (f) relaying said signal to a controller, (g) in said controller, comparing said signal to previous signals relating degree of recrystallization of said sheet product to provide a comparison, and (h) in response to said comparison, maintaining or changing said temperature in said temperature range upwardly or downwardly to produce aluminum sheet product having desired recrystallization.
- US2005/0211350 and US2013334091 are directed to a method of manufacturing T or O temper aluminum alloy sheet in an in-line sequence comprising the steps of (i) providing a thin cast aluminum alloy strip having a first thickness, (ii) quenching the strip with a first quench to a hot or warm rolling temperature, (iii) hot or warm rolling the strip to a final thickness that is about 10 to 65% reduced from the first thickness, (iv) selectively proceeding according to a first set of criteria depending on whether a T or O temper is desired and (v) quenching the strip with a second quench if a T temper is desired.
- WO 2013/133960 A1 relates to method comprising (a) preparing an aluminum alloy sheet for post-solutionizing cold work, wherein the aluminum alloy sheet includes 2.0 to 22 wt.% zinc, wherein the zinc is the predominate alloying element of the aluminum alloy sheet other than aluminum, and wherein the preparing step comprises (i) continuously casting the aluminum alloy sheet, the continuously casting step comprising (A) delivering molten aluminum metal comprising an aluminum alloy having 2.0 to 22 wt.
- % zinc wherein the zinc is the predominate alloying element of the aluminum alloy other than aluminum to a pair of spaced apart rotating casting rolls defining a nip therebetween, (B) advancing the molten metal between surfaces of the casting rolls, wherein a freeze front of metal is formed at the nip, and (C) withdrawing the aluminum alloy sheet in the form of a solid metal strip from the nip, (ii) concomitant to the continuously casting step, solutionizing the aluminum alloy sheet, (b) after the preparing step (a), cold working the aluminum alloy sheet by at least 25%, and after the cold working step (b), thermally treating the aluminum alloy sheet, wherein the cold working and the thermally treating steps are accomplished to achieve an increase in long-transverse tensile yield strength as compared to a reference-version of the aluminum alloy body in the as cold-worked condition.
- the present disclosure includes a method for producing rolled aluminum alloy articles as defined in claim 1.
- the present disclosure also includes a continuous casting system as defined in claim 10.
- rolled aluminum alloy article which is formed by the methods and systems described herein, wherein the rolled aluminum alloy article is provided in a controlled temper.
- the rolled aluminum alloy article is a thick gauge aluminum alloy article, such as, but not limited to, plates, shates, slabs, sheet plates and the like.
- Certain aspects and features of the present disclosure relate to techniques for producing thick gauge aluminum alloy articles, such as, but not limited to, plates, shates, slabs, sheet plates and the like.
- the disclosed techniques include providing a molten aluminum alloy, continuously casting an aluminum alloy article from the molten aluminum alloy, reheating (e.g., solutionizing) the cast aluminum alloy article, and hot or warm rolling the aluminum alloy article at a rolling temperature of at least about 400 °C to a gauge of 4 mm or greater to produce a thick gauge aluminum alloy article.
- the reheating can include heating the cast aluminum alloy article to a solutionizing temperature at or above the solvus temperature for the cast aluminum alloy article, although lower reheating temperatures may be used.
- the reheating can include reheating the cast aluminum alloy article to a temperature at or above a minimum peak metal temperature of at 420 °C, 425 °C, 430 °C, 435 °C, 440 °C, 445 °C, 450 °C, 455 °C, 460 °C, 465 °C, 470 °C, 475 °C, 480 °C, 485 °C, 490 °C, 495 °C, 500 °C, 505 °C, 510 °C, 515 °C, 520 °C, 525 °C, 530 °C, 535 °C, 540 °C, 545 °C, 550 °C, 555 °C, 560 °C, 565
- the reheating can include reheating an AA6xxx series cast aluminum alloy article to a peak metal temperature between 550 °C - 570 °C or 555 °C - 565 °C, or at or approximately 560 °C. In some cases, the reheating can include reheating an AA7xxx series cast aluminum alloy article to a peak metal temperature between 470 °C - 490 °C or 475 °C - 485 °C, or at or approximately 480 °C.
- the continuous casting system includes a pair of moving opposed casting surfaces and a casting cavity between the pair of moving opposed casting surfaces.
- the continuous casting system also includes a solutionizing furnace positioned downstream of the pair of moving opposed casting surfaces and a rolling mill positioned downstream of the furnace.
- the system further includes a first quenching device positioned downstream of the rolling mill and a second quenching device positioned upstream of the rolling mill.
- the system further has a shearing device positioned downstream of the first quenching device and a stacking device positioned downstream of the shearing device.
- Described herein is also an aluminum alloy article, which is formed by the methods and systems described herein and is provided in a controlled temper.
- the aluminum alloy article described herein is able to be produced more efficiently and with less cost, waste, and/or energy usage per kilogram of produced aluminum alloy article than conventional techniques.
- thick gauge articles have a thickness of about 4 mm or greater, and can include, but are not limited to, plates, shates, slabs, sheet plates and the like.
- An F condition or temper refers to an aluminum alloy as fabricated.
- An O condition or temper refers to an aluminum alloy after annealing.
- a T3 condition or temper refers to an aluminum alloy after solutionizing, cold working and natural aging.
- a T4 condition or temper refers to an aluminum alloy after solutionizing followed by natural aging.
- a T6 condition or temper refers to an aluminum alloy after solutionizing followed by artificial aging.
- a T7 condition or temper refers to an aluminum alloy after solutionizing, quenching, and artificially overaging.
- a T8 condition or temper refers to an aluminum alloy after solutionizing, followed by cold working, followed by artificial aging.
- a thick gauge aluminum alloy article such as an aluminum alloy plate, shate, slab, sheet plate or other article having a gauge of 4 mm or greater is defined in claim 1.
- the molten aluminum alloy can be an AA2xxx series aluminum alloy, an AA5xxx series aluminum alloy, an AA6xxx series aluminum alloy, or an AA7xxx series aluminum alloy.
- the aluminum alloy as described herein can be an AA2xxx aluminum alloy according to one of the following aluminum alloy designations: AA2001, A2002, AA2004, AA2005, AA2006, AA2007, AA2007A, AA2007B, AA2008, AA2009, AA2010, AA2011, AA2011A, AA2111, AA2111A, AA2111B, AA2012, AA2013, AA2014, AA2014A, AA2214, AA2015, AA2016, AA2017, AA2017A, AA2117, AA2018, AA2218, AA2618, AA2618A, AA2219, AA2319, AA2419, AA2519, AA2021, AA2022, AA2023, AA2024, AA2024A, AA2124, AA2224, AA2224A, AA2324, AA2424, AA2524, AA2624, AA2724, AA2824, AA
- the aluminum alloy as described herein can be an AA5xxx aluminum alloy according to one of the following aluminum alloy designations: AA5005, AA5005A, AA5205, AA5305, AA5505, AA5605, AA5006, AA5106, AA5010, AA5110, AA5110A, AA5210, AA5310, AA5016, AA5017, AA5018, AA5018A, AA5019, AA5019A, AA5119, AA5119A, AA5021, AA5022, AA5023, AA5024, AA5026, AA5027, AA5028, AA5040, AA5140, AA5041, AA5042, AA5043, AA5049, AA5149, AA5249, AA5349, AA5449, AA5449A, AA5050, AA5050A, AA5050C, AA5150, AA5051, AA5051
- the aluminum alloy as described herein can be an AA6xxx aluminum alloy according to one of the following aluminum alloy designations: AA6101, AA6101A, AA6101B, AA6201, AA6201A, AA6401, AA6501, AA6002, AA6003, AA6103, AA6005, AA6005A, AA6005B, AA6005C, AA6105, AA6205, AA6305, AA6006, AA6106, AA6206, AA6306, AA6008, AA6009, AA6010, AA6110, AA6110A, AA6011, AA6111, AA6012, AA6012A, AA6013, AA6113, AA6014, AA6015, AA6016, AA6016A, AA6116, AA6018, AA6019, AA6020, AA6021, AA6022, AA6023, AA6024, AA6025, AA6026,
- the aluminum alloy as described herein can be an AA7xxx aluminum alloy according to one of the following aluminum alloy designations: AA7011, AA7019, AA7020, AA7021, AA7039, AA7072, AA7075, AA7085, AA7108, AA7108A, AA7015, AA7017, AA7018, AA7019A, AA7024, AA7025, AA7028, AA7030, AA7031, AA7033, AA7035, AA7035A, AA7046, AA7046A, AA7003, AA7004, AA7005, AA7009, AA7010, AA7011, AA7012, AA7014, AA7016, AA7116, AA7122, AA7023, AA7026, AA7029, AA7129, AA7229, AA7032, AA7033, AA7034, AA7036, AA71
- Figure 1 is a process flowchart 10 depicting the method for producing thick gauge aluminum alloy articles, such as plates, shates, slabs, sheet plates or other articles having a gauge of about 4 mm or greater.
- thin gauge casting refers to continuously casting an aluminum alloy article.
- continuously casting an aluminum alloy article can replace a conventional method of direct chill casting an aluminum alloy ingot.
- the continuous casting can be performed by any suitable continuous caster such as a twin belt caster, twin block caster or twin roll caster.
- the aluminum alloy article as cast has a thickness of from about 50 mm to about 5 mm.
- a continuously cast aluminum alloy article can have a gauge thickness of at or about 50 mm, 45 mm, 40 mm, 35 mm, 30 mm, 25 mm, 20 mm, 15 mm, 10 mm, 5 mm, or anywhere in between, upon exiting the continuous caster.
- the aluminum alloy article is cast to a gauge between about 15 mm to about 25 mm.
- the aluminum alloy article is cast to a gauge of from about 15 mm to about 40 mm.
- casting a thinner gauge cast aluminum alloy article directly from a molten alloy can significantly reduce processing time and cost.
- the aluminum alloy article upon exiting a continuous casting device, can have a caster exit temperature of from at or about 350 °C to at or about 500 °C.
- the aluminum alloy article can have a caster exit temperature of at or about 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, or anywhere in between.
- the aluminum alloy article is reheated at block 30.
- reheating at block 30 can include solutionizing.
- Solutionizing can refer to a thermal treatment employed to evenly distribute alloying elements throughout an aluminum matrix within the aluminum alloy article (e.g., create a solid solution).
- solutionizing a continuously cast aluminum alloy article can be performed more efficiently than solutionizing an aluminum alloy plate created from an aluminum alloy ingot.
- Solutionizing an aluminum alloy plate created from an aluminum alloy ingot is typically performed by heating the aluminum alloy plate created from the ingot to a solutionization temperature of about 560 °C and soaking the aluminum alloy plate at a temperature of about 560 °C for up to about 1 hour.
- Reheating a continuously cast aluminum alloy article as disclosed herein is performed at a peak metal temperature of from at 420 °C to at 580 °C (e.g., at 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, 570 °C, 580 °C, or anywhere in between) having a soak time of less than 5 minutes (e.g., less than 5 minutes, less than 4 minutes, less than 3 minutes, less than 2 minutes, less than 1 minute, or anywhere in between).
- reheating a continuously cast aluminum alloy article is performed at about 560 °C for less than about 3 minutes. In some aspects, decreasing the reheating temperature can require increasing the soak time, and vice versa.
- the aluminum alloy article can have a furnace exit temperature of from at or about 420 °C to at or about 580 °C (e.g., at or about 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, 570 °C, 580 °C, or anywhere in between).
- the furnace can be employed to maintain the caster exit temperature of the aluminum alloy article during passage from the continuous casting device to the rolling mill.
- hot rolling to final gauge refers to reducing the gauge thickness of the aluminum alloy article to produce an aluminum alloy article having a desired thickness (e.g., gauge). In some cases, hot rolling to final gauge results in a thick gauge aluminum alloy article (e.g., having a thickness of 4 mm or greater such as, but not limited to, between 4 mm and about 15 mm or between about 6 mm and about 15 mm). In some cases, hot rolling a continuously cast aluminum alloy article to a final gauge can be performed more efficiently than a comparative method of breaking down an aluminum alloy ingot from a thickness of from about 450 mm to about 600 mm to a thickness of 4 mm or greater.
- hot rolling a continuously cast aluminum alloy article from a gauge of from about 15 mm to about 40 mm to a final gauge of 4 mm or greater can be performed in a single pass through a hot rolling mill.
- the aluminum alloy article is hot rolled to a gauge between 4 mm and about 15 mm or between about 6 mm and about 15 mm.
- the percentage reduction in thickness in a single pass through the hot rolling mill can be at or about at least 35%, 40%, 45%, 50%, 55%, 60%, 65%, or 70%.
- hot rolling a continuously cast aluminum alloy article from a gauge between at or about 15 mm and 40 mm to a final gauge of 4 mm or greater can be performed at a temperature of from about 400 °C to about 480 °C (e.g., at or about 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, or anywhere in between) and the aluminum alloy article can have a hot rolling mill entry temperature of from at or about 350 °C to at or about 560 °C.
- an aluminum alloy article can have a hot rolling mill entry temperature of at or about 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, or anywhere in between.
- the aluminum alloy article can exit the furnace (e.g., solutionizing furnace) having a temperature of at or about 560 °C and have a hot rolling mill entry temperature of at or about 530 °C.
- hot rolling is performed at a temperature as hot as possible without melting the aluminum alloy article.
- the aluminum alloy article can be subjected to hot rolling (e.g., reduction in thickness) from an as-continuously-cast gauge to a final gauge without any cold rolling.
- hot rolling e.g., reduction in thickness
- the aluminum alloy article can be reduced to a thick gauge aluminum article, such as 4 mm or greater, such as a aluminum alloy plate, shate, slab, sheet plate, etc.
- the aluminum alloy gauge can be reduced by from about 0% to about 88%.
- the aluminum alloy article can be subjected to a reduction in gauge of 0%, 2%, 4%, 6%, 8%, 10%, 12%, 14%, 16%, 18%, 20%, 22%, 24%, 26%, 28%, 30%, 32%, 34%, 36%, 38%, 40%, 42%, 44%, 46%, 48%, 50%, 52%, 54%, 56%, 58%, 60%, 62%, 64%, 66%, 68%, 70%, 72%, 74%, 76%, 78%, 80%, 82%, 84%, 86%, 88%, or anywhere in between.
- the reduction in thickness at block 40 can be at least at or about 35%, 36%, 37%, 38%, 39%, 40%, 41%, 42%, 43%, 44%, 45%, 46%, 47%, 48%, 49%, or 50%.
- the aluminum alloy article can be hot rolled to a final gauge of 4 mm or greater, such as between 4 mm and 15 mm or between about 6 mm and about 15 mm.
- the final gauge of the thick gauge aluminum alloy article is 4 mm, 5 mm, 6 mm, 7 mm, 8 mm, 9 mm, 10 mm, 11 mm, 12 mm, 13 mm, 14 mm, or 15 mm, or anywhere in between.
- the rolled aluminum alloy article can have a hot rolling mill exit temperature of from at about 380 °C to at about 450 °C.
- the aluminum alloy article can have a hot rolling mill exit temperature of at about 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, or anywhere in between.
- the aluminum alloy article has a hot rolling mill exit temperature of at about 400 °C.
- the aluminum alloy article is thermally quenched upon exiting the rolling mill. Quenching can be performed with water and/or forced air. In some non-limiting examples, quenching is performed by spraying water onto at least a first side of the aluminum alloy article. In some cases, quenching is performed by spraying water onto a first side of the aluminum alloy article and a second side of the aluminum alloy article. In some aspects, the aluminum alloy article can be quenched by immersion in water. In some non-limiting examples, quenching can be performed at a rate of at least at or about 100 °C/second (°C/s).
- quenching can be performed at a rate of at or about 100 °C/s, 120 °C/s, 140 °C/s, 160 °C/s, 180 °C/s, 200 °C/s, 220 °C/s, 240 °C/s, 260 °C/s, or anywhere in between.
- the aluminum alloy article can be quenched to or below a temperature between at or about 200 °C and 130 °C.
- the aluminum alloy article can be quenched to a temperature of at or about 200 °C or below, at or about 190 °C or below, at or about 180 °C or below, at or about 170 °C or below, at or about 160 °C or below, at or about 150 °C or below, at or about 140 °C or below, at or about 130 °C or below, or anywhere in between.
- Quenching is performed before rolling (e.g., to perform a lower temperature rolling, sometimes referred to as warm rolling) and after rolling. In some further cases, only minimal quenching is performed (e.g., the aluminum alloy article can be minimally quenched to a temperature of at or about 395 °C or below, at or about 390 °C or below, at or about 385 °C or below, at or about 380 °C or below, at or about 375 °C or below, at or about 370 °C or below, at or about 365 °C or below, at or about 360 °C or below, or anywhere in between, upon exiting the hot rolling mill).
- Warm rolling to final gauge can refer to reducing the gauge thickness of the aluminum alloy article at a temperature less than hot rolling to produce a thick gauge aluminum alloy article having a desired gauge (e.g., about 4 mm or greater, such as between about 4 mm and about 15 mm or between about 6 mm and about 15 mm), wherein the reduction occurs at a temperature between cold rolling and hot rolling (e.g., below a recrystallization temperature).
- a desired gauge e.g., about 4 mm or greater, such as between about 4 mm and about 15 mm or between about 6 mm and about 15 mm
- warm rolling a continuously cast aluminum alloy article to a final gauge can be performed to produce a thick gauge aluminum alloy article having a temper similar to any suitable temper achieved by performing cold rolling.
- warm rolling a continuously cast aluminum alloy article from a gauge between at or about 15 mm and 40 mm to a final gauge of 4 mm or greater can be performed in a single pass through a warm rolling mill (e.g., a hot rolling mill operating at lower temperatures).
- warm rolling a continuously cast aluminum alloy article from a gauge of from at or about 15 mm to at or about 40 mm to a final gauge of from 4 mm or greater can be performed at a temperature of from at or about 300 °C to at or about 400 °C (e.g., at or about 300 °C, 310 °C, 320 °C, 330 °C, 340 °C, 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, or anywhere in between) and the aluminum alloy article can have a rolling mill entry temperature for warm rolling of from at or about 350 °C to at or about 480 °C.
- a thick gauge aluminum alloy article can have a rolling mill entry temperature of at or about 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, or anywhere in between.
- the thick gauge aluminum alloy article can exit the furnace (e.g., solutionizing furnace) at a temperature of at or about 560 °C and be subjected to quenching to a temperature of from at or about 300 °C to at or about 480 °C (e.g., at or about 300 °C, 310 °C, 320 °C, 330 °C, 340 °C, 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, or anywhere in between).
- the thick gauge aluminum alloy article can have a rolling mill entry temperature for warm rolling of less than at or about 480 °C. In some non-limiting examples, warm rolling is performed at a temperature of less than at or about 350 °C.
- the aluminum alloy article can be subjected to warm rolling (e.g., reduction in thickness) from an as-continuously-cast gauge to a final gauge.
- the aluminum alloy article can be reduced to a thick gauge aluminum alloy article, for example an aluminum alloy article having a thickness of 4 mm or greater (such as, but not limited to, between 4 mm and about 15 mm or between about 6 mm and about 15 mm).
- the aluminum alloy gauge can be reduced by from about 0% to about 88%.
- the aluminum alloy article can be subjected to a reduction in gauge of 0%, 2%, 4%, 6%, 8%, 10%, 12%, 14%, 16%, 18%, 20%, 22%, 24%, 26%, 28%, 30%, 32%, 34%, 36%, 38%, 40%, 42%, 44%, 46%, 48%, 50%, 52%, 54%, 56%, 58%, 60%, 62%, 64%, 66%, 68%, 70%, 72%, 74%, 76%, 78%, 80%, 82%, 84%, 86%, 88%, or anywhere in between.
- the reduction in thickness at block 40 can be at least at or about 35%, 36%, 37%, 38%, 39%, 40%, 41%, 42%, 43%, 44%, 45%, 46%, 47%, 48%, 49%, or 50%.
- the aluminum alloy article can be warm rolled to a final gauge of 4 mm or greater. In some examples, the article is warm rolled to a final gauge between 4 mm and about 15 mm or between about 6 mm and about 15 mm.
- the aluminum alloy article can be reheated (e.g., solutionized) after hot or warm rolling.
- reheating a hot or warm rolled continuously cast aluminum alloy article as disclosed herein can be performed at a peak metal temperature of from at or about 420 °C to at or about 580 °C (e.g., at or about 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, 570 °C, 580 °C, or anywhere in between) having a soak time of less than about 5 minutes (e.g., less than about 5 minutes, less than about 4 minutes, less than about 3 minutes, less than about 2 minutes, less than about 1 minute, or anywhere in between).
- reheating a continuously cast aluminum alloy article is performed at about 560 °C for less than about 3 minutes. In some aspects, decreasing the reheating temperature can require increasing the soak time, and vice versa.
- the aluminum alloy article can have a furnace exit temperature of from at or about 420 °C to at or about 580 °C (e.g., at or about 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, 570 °C, 580 °C, or anywhere in between). In some cases, reheating is not performed after hot or warm rolling.
- cutting to length refers to cutting the rolled thick gauge aluminum alloy articles to a desired length (e.g., as requested by a customer) in-situ after quenching.
- aluminum alloy material is not coiled for post-production applications including storage, aging and shipping, to name a few.
- the thick gauge aluminum alloy articles in some examples, aluminum alloy plates, shates, slabs, sheet plates or the like
- the thick gauge aluminum alloy articles can have a stacking temperature of from at or about 100 °C or below to at or about 250 °C or below.
- the thick gauge aluminum alloy articles can be stacked at or below a temperature of at or about 100 °C, 110 °C, 120 °C, 130 °C, 140 °C, 150 °C, 160 °C, 170 °C, 180 °C, 190 °C, 200 °C, 210 °C, 220 °C, 230 °C, 240 °C, 250 °C, or anywhere in between.
- the stacking temperature can affect a temper of the thick gauge aluminum alloy articles.
- stacking solutionized thick gauge aluminum alloy articles at a stacking temperature of at or about 100 °C can result in thick gauge aluminum alloy articles having a T4 temper.
- stacking solutionized AA6xxx series thick gauge aluminum alloy articles at a stacking temperature of at or about 200 °C can result in AA6xxx thick gauge aluminum alloy articles having a T6 temper.
- stacking the same AA6xxx thick gauge aluminum alloy articles at a stacking temperature of at or about 250 °C can result in AA6xxx thick gauge aluminum alloy articles having a T7 temper.
- stacking solutionized AA7xxx series thick gauge aluminum alloy articles at a stacking temperature of at or about 165 °C and maintaining that temperature for at or about 24 hours can provide AA7xxx series thick gauge aluminum alloy articles having a T7 temper.
- Other stacking temperatures and times can be used to affect the temper of the thick gauge aluminum alloy articles as appropriate.
- artificial aging can refer to a thermal treatment process that can impart desired tempers to provided thick gauge aluminum alloy articles (in some examples, aluminum alloy plates, shates, slabs, sheet plates or the like).
- desired tempers in some examples, aluminum alloy plates, shates, slabs, sheet plates or the like.
- artificial aging is accomplished as part of the stacking process, such as described above.
- artificial aging is performed by further subjecting the thick gauge aluminum alloy articles to an elevated temperature suitable for artificial aging.
- Figure 2 is a schematic diagram depicting a continuous casting system 100 according to certain aspects and features of the present disclosure.
- a pair of moving opposed casting surfaces 110 define a casting cavity 115 between the pair of moving opposed casting surfaces 110.
- the pair of moving opposed casting surfaces 110 can be a twin roll caster or a twin belt caster, or any other suitable continuous casting device.
- a molten metal injector positioned upstream of the pair of moving opposed casting surfaces 110 can inject molten metal (e.g., a molten aluminum alloy) into the casting cavity 115 between the pair of moving opposed casting surfaces 110.
- the pair of moving opposed casting surfaces 110 can cast the molten aluminum alloy into a metal article, for example, an aluminum alloy article 120.
- Casting the molten aluminum alloy into an aluminum alloy article 120 can include rapidly extracting heat from the molten aluminum alloy as the molten aluminum alloy article moves through the casting cavity 115 and the aluminum alloy article 120 exits the casting cavity 115.
- a furnace 130 positioned downstream of the pair of moving opposed casting surfaces 110 is employed to reheat the aluminum alloy article 120.
- the furnace 130 is a solutionizing furnace, which can be employed to solutionize the aluminum alloy article 120.
- the furnace 130 can be employed to maintain the cast exit temperature of the aluminum alloy article 120.
- the furnace 130 can operate at a temperature above the cast exit temperature of the aluminum alloy article 120, in which case optional heating elements positioned upstream of the furnace 130 can increase the temperature of the aluminum alloy article 120 before it enters the furnace 130.
- a rolling mill 140 positioned downstream of the furnace 130 can be used to reduce the thickness of the aluminum alloy article 120, resulting in a thick gauge aluminum alloy article 125 (e.g., the rolling mill 140 can roll the aluminum alloy article 120 into a thick gauge aluminum alloy article 125).
- a quenching device 160 positioned downstream of the rolling mill 140 is used to quench (e.g., rapidly cool) the thick gauge aluminum alloy article 125.
- a plate shearing device 170 positioned downstream of the quenching device 160 can be employed to cut the thick gauge aluminum alloy article 125 to a desired length. If desired, the cut thick gauge aluminum alloy article 125 is then stacked into a stack 180 of thick gauge aluminum alloy articles 125 for any suitable further downstream processing.
- a second quenching device 165 is positioned upstream of the rolling mill 140 to quench the aluminum alloy article 120 prior to rolling.
- a second quenching device 165 can be suitable for use with a warm rolling procedure (e.g., rolling at temperatures below the recrystallization temperature).
- the use of a second quenching device 165 immediately before rolling can result in the thick gauge aluminum alloy article 125 having mechanical properties similar to aluminum alloy rolled articles having a T3 or a T8 temper (e.g., high strength, and precipitation hardened).
- the methods described above can provide thick gauge aluminum alloy articles (e.g., plates, shates, slabs, sheet plates, etc.) having mechanical properties similar to aluminum alloy articles produced via cold working (e.g., cold rolling) even though the thick gauge aluminum alloy articles described herein are not cold rolled.
- mechanical properties exhibited by aluminum alloys having a T3 or a T8 temper as described above can be imparted to the thick gauge aluminum alloy articles described herein using the methods described herein.
- T8 temper properties are desired, an aluminum alloy can be subjected to continuous casting, solutionizing, quenching, hot rolling to a final gauge and quenching after hot rolling, described in detail below.
- the continuous casting system 100 can be arranged in a plurality of configurations to provide a specifically-tailored thermal history for the thick gauge aluminum alloy articles 125. Described herein is that an AA6xxx series aluminum alloy in T4, T6, or T7 temper can be produced by casting an aluminum alloy article 120 such that the aluminum alloy article 120 exiting the casting cavity 115 has a caster exit temperature of about 450 °C, solutionizing in the solutionizing furnace 130 at a temperature of about 560 °C, and subjecting the aluminum alloy article 120 to a 50% reduction in the rolling mill 140 at a temperature between approximately 530 °C and 580 °C.
- the thick gauge aluminum alloy article 125 can exit the rolling mill 140 and be immediately quenched using a quenching device 160 to a temperature at or below 200 °C, then cut using cutting device 160 and stacked at a temperature at or below 100 °C.
- the thick gauge aluminum alloy article 125 can exit the rolling mill 140 and be immediately quenched using a quenching device 160 to a temperature at or about 200 °C, then cut using cutting device 160 and stacked at a temperature at or about 200 °C.
- the thick gauge aluminum alloy article 125 can exit the rolling mill 140 and be immediately quenched using a quenching device 160 to a temperature at or about 250 °C, then cut using cutting device 160 and stacked at a temperature at or about 250 °C.
- an AA6xxx series aluminum alloy having T3 or T8 temper properties can be produced without cold rolling.
- the AA6xxx series aluminum alloy having T3 or T8 temper properties can be provided by casting an aluminum alloy article 120 such that the aluminum alloy article 120 exiting the casting cavity 115 has a caster exit temperature of about 450 °C, solutionizing in the solutionizing furnace 130 at a temperature of about 560 °C, then quenching the aluminum alloy article 120 using quenching device 165 to a temperature of about 470 °C before subjecting the aluminum alloy article 120 to a 50% reduction in the rolling mill 140 at a temperature below approximately 500 °C, such as at or about 470 °C.
- the resultant thick gauge aluminum alloy article 125 can exit the rolling mill 140 at a rolling mill exit temperature of about 400 °C and be immediately quenched using quenching device 160 to a temperature of at or below about 200 °C.
- the thick gauge aluminum alloy article 125 can be cut using cutting device 160 and stacked at a temperature at or below 100 °C.
- the thick gauge aluminum alloy article 125 can be cut using cutting device 160 and stacked at a temperature at or about 200 °C.
- the thick gauge aluminum alloy article 125 can be cut using cutting device 160, stacked at a temperature at or about 200 °C, and artificially aged.
- Alloy A and Alloy B (see Table 1) were provided in a T4 temper, a partial T6 temper, and a full T6 temper by employing the methods described above and optional artificial aging.
- Alloy A and Alloy B can be produced by the methods depicted in Figure 1 , including casting an aluminum alloy article such that the aluminum alloy article exiting the casting cavity 115 has a caster exit temperature of about 450 °C, solutionizing in the solutionizing furnace 130 at a temperature of from about 550 °C to about 570 °C for 2 minutes, and subjecting the aluminum alloy article 120 to about a 40% to about a 70% reduction in the rolling mill 140 at a temperature between approximately 530 °C and 580 °C.
- Alloy A was reduced about 40% to a gauge of 9.5 mm. Alloy B was reduced about 70% to a gauge of 5.0 mm.
- a thick gauge aluminum alloy article can exit the rolling mill 140 and be immediately quenched using the quenching device 160 to a temperature at or below 50 °C, then cut using the cutting device 160 and stacked at a temperature at or below 100 °C.
- the thick gauge aluminum alloy articles can be artificially aged at 200 °C for 2 hours.
- the thick gauge aluminum alloy articles can be artificially aged at 180 °C for 10 hours.
- Figure 3 is a chart depicting mechanical properties of thick gauge aluminum alloy articles made from Alloy A and Alloy B. Both Alloy A and Alloy B exhibited high strength after artificial aging (e.g., in partial T6 temper and full T6 temper) having yield strength (referred to as "YS" in Figure 3 ) (left histogram in each group) of from about 330 MPa to about 345 MPa.
- YS yield strength
- Both Alloy A and Alloy B exhibited ample strength after natural aging (e.g., in T4 temper) having yield strength (left histogram in each group) of from about 180 MPa to about 200 MPa, and excellent deformability (e.g., uniform elongation, referred to as "UE" in Figure 3 and represented by open circles) of about 21% to about 22% UE.
- yield strength left histogram in each group
- deformability e.g., uniform elongation, referred to as "UE” in Figure 3 and represented by open circles
- having a UE of about 21% to about 22% can allow a 90° bend during forming (e.g., stamping, or bending) without fracture or failure.
- Alloy A and Alloy B exhibited high ultimate tensile strengths (referred to as “UTS” in Figure 3 ) (right histogram in each group), as well as high total elongation before fracture (referred to as "TE” in Figure 3 and represented by open diamonds).
- UTS ultimate tensile strengths
- TE high total elongation before fracture
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Description
- This application claims the benefit of
U.S. Provisional Application Nos. 62/529,028, filed July 6, 2017 62/413,740, filed October 27, 2016 62/413,764, filed October 27, 2016 62/413,591, filed October 27, 2016 62/505,944, filed May 14, 2017 - Additionally, the present application is related to
U.S. Non-Provisional Patent Application No. 15/717,361 to Milan Felberbaum et al. - The present disclosure relates to metallurgy generally and more specifically to metal plate manufacturing.
- Current methods of producing thick gauge (e.g., greater than 4 millimeters (mm) in thickness) aluminum alloy articles require numerous processing steps including subjecting a nascent aluminum alloy body to thermal treatment processes for long durations. It can be desirable to reduce the number of steps and overall time required to produce aluminum alloy articles with desirable thermal treatment.
-
US 2003/0150587 A1 is directed to a process for producing an aluminum sheet product having a controlled recrystallization using a continuous caster to cast a molten aluminum alloy into a slab comprising (a) providing a source of molten aluminum alloy, (b) providing a caster for continuously casting said molten aluminum alloy into a slab, (c) rolling said slab into a sheet product, (d) continuously annealing said sheet product at a temperature in a controlled temperature range, (e) measuring degree of recrystallization of said sheet product on a continuous basis to provide a recrystallization related signal, (f) relaying said signal to a controller, (g) in said controller, comparing said signal to previous signals relating degree of recrystallization of said sheet product to provide a comparison, and (h) in response to said comparison, maintaining or changing said temperature in said temperature range upwardly or downwardly to produce aluminum sheet product having desired recrystallization. -
US2005/0211350 andUS2013334091 are directed to a method of manufacturing T or O temper aluminum alloy sheet in an in-line sequence comprising the steps of (i) providing a thin cast aluminum alloy strip having a first thickness, (ii) quenching the strip with a first quench to a hot or warm rolling temperature, (iii) hot or warm rolling the strip to a final thickness that is about 10 to 65% reduced from the first thickness, (iv) selectively proceeding according to a first set of criteria depending on whether a T or O temper is desired and (v) quenching the strip with a second quench if a T temper is desired. -
WO 2013/133960 A1 relates to method comprising (a) preparing an aluminum alloy sheet for post-solutionizing cold work, wherein the aluminum alloy sheet includes 2.0 to 22 wt.% zinc, wherein the zinc is the predominate alloying element of the aluminum alloy sheet other than aluminum, and wherein the preparing step comprises (i) continuously casting the aluminum alloy sheet, the continuously casting step comprising (A) delivering molten aluminum metal comprising an aluminum alloy having 2.0 to 22 wt. % zinc, wherein the zinc is the predominate alloying element of the aluminum alloy other than aluminum to a pair of spaced apart rotating casting rolls defining a nip therebetween, (B) advancing the molten metal between surfaces of the casting rolls, wherein a freeze front of metal is formed at the nip, and (C) withdrawing the aluminum alloy sheet in the form of a solid metal strip from the nip, (ii) concomitant to the continuously casting step, solutionizing the aluminum alloy sheet, (b) after the preparing step (a), cold working the aluminum alloy sheet by at least 25%, and after the cold working step (b), thermally treating the aluminum alloy sheet, wherein the cold working and the thermally treating steps are accomplished to achieve an increase in long-transverse tensile yield strength as compared to a reference-version of the aluminum alloy body in the as cold-worked condition. - The term embodiment and like terms are intended to refer broadly to all of the subject matter of this disclosure and the claims below. Statements containing these terms should be understood not to limit the subject matter described herein or to limit the meaning or scope of the claims below. Embodiments of the present disclosure covered herein are defined by the claims below, not this summary. This summary is a high-level overview of various aspects of the disclosure and introduces some of the concepts that are further described in the Detailed Description section below. This summary is not intended to identify key or essential features of the claimed subject matter, nor is it intended to be used in isolation to determine the scope of the claimed subject matter. The subject matter should be understood by reference to appropriate portions of the entire specification of this disclosure, any or all drawings and each claim.
- The present disclosure includes a method for producing rolled aluminum alloy articles as defined in claim 1.
- The present disclosure also includes a continuous casting system as defined in
claim 10. - Described herein is also a rolled aluminum alloy article, which is formed by the methods and systems described herein, wherein the rolled aluminum alloy article is provided in a controlled temper. In some cases, the rolled aluminum alloy article is a thick gauge aluminum alloy article, such as, but not limited to, plates, shates, slabs, sheet plates and the like.
- The specification makes reference to the following appended figures, in which use of like reference numerals in different figures is intended to illustrate like or analogous components.
-
Figure 1 is a flowchart depicting a process for producing an aluminum alloy article according to certain aspects of the present disclosure. -
Figure 2 is a schematic diagram depicting a processing line according to certain aspects of the present disclosure. -
Figure 3 is a chart depicting mechanical properties of aluminum alloy articles according to certain aspects of the present disclosure. - Certain aspects and features of the present disclosure relate to techniques for producing thick gauge aluminum alloy articles, such as, but not limited to, plates, shates, slabs, sheet plates and the like. The disclosed techniques include providing a molten aluminum alloy, continuously casting an aluminum alloy article from the molten aluminum alloy, reheating (e.g., solutionizing) the cast aluminum alloy article, and hot or warm rolling the aluminum alloy article at a rolling temperature of at least about 400 °C to a gauge of 4 mm or greater to produce a thick gauge aluminum alloy article.
- In some cases, the reheating can include heating the cast aluminum alloy article to a solutionizing temperature at or above the solvus temperature for the cast aluminum alloy article, although lower reheating temperatures may be used. In some cases, the reheating can include reheating the cast aluminum alloy article to a temperature at or above a minimum peak metal temperature of at 420 °C, 425 °C, 430 °C, 435 °C, 440 °C, 445 °C, 450 °C, 455 °C, 460 °C, 465 °C, 470 °C, 475 °C, 480 °C, 485 °C, 490 °C, 495 °C, 500 °C, 505 °C, 510 °C, 515 °C, 520 °C, 525 °C, 530 °C, 535 °C, 540 °C, 545 °C, 550 °C, 555 °C, 560 °C, 565 °C, 570 °C, 575 °C, or 580 °C. In some cases, the reheating can include reheating an AA6xxx series cast aluminum alloy article to a peak metal temperature between 550 °C - 570 °C or 555 °C - 565 °C, or at or approximately 560 °C. In some cases, the reheating can include reheating an AA7xxx series cast aluminum alloy article to a peak metal temperature between 470 °C - 490 °C or 475 °C - 485 °C, or at or approximately 480 °C.
- Certain aspects and features of the present disclosure further relate to a continuous casting system. The continuous casting system includes a pair of moving opposed casting surfaces and a casting cavity between the pair of moving opposed casting surfaces. The continuous casting system also includes a solutionizing furnace positioned downstream of the pair of moving opposed casting surfaces and a rolling mill positioned downstream of the furnace. The system further includes a first quenching device positioned downstream of the rolling mill and a second quenching device positioned upstream of the rolling mill. The system further has a shearing device positioned downstream of the first quenching device and a stacking device positioned downstream of the shearing device.
- Described herein is also an aluminum alloy article, which is formed by the methods and systems described herein and is provided in a controlled temper. In some cases, the aluminum alloy article described herein is able to be produced more efficiently and with less cost, waste, and/or energy usage per kilogram of produced aluminum alloy article than conventional techniques.
- The terms "invention," "the invention," "this invention" and "the present invention" used herein are intended to refer broadly to all of the subject matter of this patent application and the claims below. Statements containing these terms should be understood not to limit the subject matter described herein or to limit the meaning or scope of the patent claims below.
- As used herein, the meaning of "a," "an," or "the" includes singular and plural references unless the context clearly dictates otherwise.
- In this description, reference is made to alloys identified by aluminum industry designations, such as "series" or "AA6xxx." For an understanding of the number designation system most commonly used in naming and identifying aluminum and its alloys, see "International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys" or "Registration Record of Aluminum Association Alloy Designations and Chemical Compositions Limits for Aluminum Alloys in the Form of Castings and Ingot," both published by The Aluminum Association.
- As used herein, thick gauge articles have a thickness of about 4 mm or greater, and can include, but are not limited to, plates, shates, slabs, sheet plates and the like.
- Reference is made in this application to alloy temper or condition. For an understanding of the alloy temper descriptions most commonly used, see "American National Standards (ANSI) H35 on Alloy and Temper Designation Systems." An F condition or temper refers to an aluminum alloy as fabricated. An O condition or temper refers to an aluminum alloy after annealing. A T3 condition or temper refers to an aluminum alloy after solutionizing, cold working and natural aging. A T4 condition or temper refers to an aluminum alloy after solutionizing followed by natural aging. A T6 condition or temper refers to an aluminum alloy after solutionizing followed by artificial aging. A T7 condition or temper refers to an aluminum alloy after solutionizing, quenching, and artificially overaging. A T8 condition or temper refers to an aluminum alloy after solutionizing, followed by cold working, followed by artificial aging.
- All ranges disclosed herein are to be understood to encompass any and all subranges subsumed therein. For example, a stated range of "1 to 10" should be considered to include any and all subranges between (and inclusive of) the minimum value of 1 and the maximum value of 10; that is, all subranges beginning with a minimum value of 1 or more, e.g. 1 to 6.1, and ending with a maximum value of 10 or less, e.g., 5.5 to 10.
- These illustrative examples are given to introduce the reader to the general subject matter discussed here and are not intended to limit the scope of the disclosed concepts. The following sections describe various additional features and examples with reference to the drawings in which like numerals indicate like elements, and directional descriptions are used to describe the illustrative embodiments but, like the illustrative embodiments, should not be used to limit the present disclosure. The elements included in the illustrations herein may not be drawn to scale.
- The method for producing thick gauge aluminum alloy articles, for example, a thick gauge aluminum alloy article such as an aluminum alloy plate, shate, slab, sheet plate or other article having a gauge of 4 mm or greater is defined in claim 1.
- In some cases, the molten aluminum alloy can be an AA2xxx series aluminum alloy, an AA5xxx series aluminum alloy, an AA6xxx series aluminum alloy, or an AA7xxx series aluminum alloy.
- Optionally, the aluminum alloy as described herein can be an AA2xxx aluminum alloy according to one of the following aluminum alloy designations: AA2001, A2002, AA2004, AA2005, AA2006, AA2007, AA2007A, AA2007B, AA2008, AA2009, AA2010, AA2011, AA2011A, AA2111, AA2111A, AA2111B, AA2012, AA2013, AA2014, AA2014A, AA2214, AA2015, AA2016, AA2017, AA2017A, AA2117, AA2018, AA2218, AA2618, AA2618A, AA2219, AA2319, AA2419, AA2519, AA2021, AA2022, AA2023, AA2024, AA2024A, AA2124, AA2224, AA2224A, AA2324, AA2424, AA2524, AA2624, AA2724, AA2824, AA2025, AA2026, AA2027, AA2028, AA2028A, AA2028B, AA2028C, AA2029, AA2030, AA2031, AA2032, AA2034, AA2036, AA2037, AA2038, AA2039, AA2139, AA2040, AA2041, AA2044, AA2045, AA2050, AA2055, AA2056, AA2060, AA2065, AA2070, AA2076, AA2090, AA2091, AA2094, AA2095, AA2195, AA2295, AA2196, AA2296, AA2097, AA2197, AA2297, AA2397, AA2098, AA2198, AA2099, or AA2199.
- Optionally, the aluminum alloy as described herein can be an AA5xxx aluminum alloy according to one of the following aluminum alloy designations: AA5005, AA5005A, AA5205, AA5305, AA5505, AA5605, AA5006, AA5106, AA5010, AA5110, AA5110A, AA5210, AA5310, AA5016, AA5017, AA5018, AA5018A, AA5019, AA5019A, AA5119, AA5119A, AA5021, AA5022, AA5023, AA5024, AA5026, AA5027, AA5028, AA5040, AA5140, AA5041, AA5042, AA5043, AA5049, AA5149, AA5249, AA5349, AA5449, AA5449A, AA5050, AA5050A, AA5050C, AA5150, AA5051, AA5051A, AA5151, AA5251, AA5251A, AA5351, AA5451, AA5052, AA5252, AA5352, AA5154, AA5154A, AA5154B, AA5154C, AA5254, AA5354, AA5454, AA5554, AA5654, AA5654A, AA5754, AA5854, AA5954, AA5056, AA5356, AA5356A, AA5456, AA5456A, AA5456B, AA5556, AA5556A, AA5556B, AA5556C, AA5257, AA5457, AA5557, AA5657, AA5058, AA5059, AA5070, AA5180, AA5180A, AA5082, AA5182, AA5083, AA5183, AA5183A, AA5283, AA5283A, AA5283B, AA5383, AA5483, AA5086, AA5186, AA5087, AA5187, or AA5088.
- Optionally, the aluminum alloy as described herein can be an AA6xxx aluminum alloy according to one of the following aluminum alloy designations: AA6101, AA6101A, AA6101B, AA6201, AA6201A, AA6401, AA6501, AA6002, AA6003, AA6103, AA6005, AA6005A, AA6005B, AA6005C, AA6105, AA6205, AA6305, AA6006, AA6106, AA6206, AA6306, AA6008, AA6009, AA6010, AA6110, AA6110A, AA6011, AA6111, AA6012, AA6012A, AA6013, AA6113, AA6014, AA6015, AA6016, AA6016A, AA6116, AA6018, AA6019, AA6020, AA6021, AA6022, AA6023, AA6024, AA6025, AA6026, AA6027, AA6028, AA6031, AA6032, AA6033, AA6040, AA6041, AA6042, AA6043, AA6151, AA6351, AA6351A, AA6451, AA6951, AA6053, AA6055, AA6056, AA6156, AA6060, AA6160, AA6260, AA6360, AA6460, AA6460B, AA6560, AA6660, AA6061, AA6061A, AA6261, AA6361, AA6162, AA6262, AA6262A, AA6063, AA6063A, AA6463, AA6463A, AA6763, A6963, AA6064, AA6064A, AA6065, AA6066, AA6068, AA6069, AA6070, AA6081, AA6181, AA6181A, AA6082, AA6082A, AA6182, AA6091, or AA6092.
- Optionally, the aluminum alloy as described herein can be an AA7xxx aluminum alloy according to one of the following aluminum alloy designations: AA7011, AA7019, AA7020, AA7021, AA7039, AA7072, AA7075, AA7085, AA7108, AA7108A, AA7015, AA7017, AA7018, AA7019A, AA7024, AA7025, AA7028, AA7030, AA7031, AA7033, AA7035, AA7035A, AA7046, AA7046A, AA7003, AA7004, AA7005, AA7009, AA7010, AA7011, AA7012, AA7014, AA7016, AA7116, AA7122, AA7023, AA7026, AA7029, AA7129, AA7229, AA7032, AA7033, AA7034, AA7036, AA7136, AA7037, AA7040, AA7140, AA7041, AA7049, AA7049A, AA7149, AA7249, AA7349, AA7449, AA7050, AA7050A, AA7150, AA7250, AA7055, AA7155, AA7255, AA7056, AA7060, AA7064, AA7065, AA7068, AA7168, AA7175, AA7475, AA7076, AA7178, AA7278, AA7278A, AA7081, AA7181, AA7185, AA7090, AA7093, AA7095, and AA7099.
-
Figure 1 is aprocess flowchart 10 depicting the method for producing thick gauge aluminum alloy articles, such as plates, shates, slabs, sheet plates or other articles having a gauge of about 4 mm or greater. Inbox 20, thin gauge casting refers to continuously casting an aluminum alloy article. In some aspects, continuously casting an aluminum alloy article can replace a conventional method of direct chill casting an aluminum alloy ingot. The continuous casting can be performed by any suitable continuous caster such as a twin belt caster, twin block caster or twin roll caster. In some examples, the aluminum alloy article as cast has a thickness of from about 50 mm to about 5 mm. For example, a continuously cast aluminum alloy article can have a gauge thickness of at or about 50 mm, 45 mm, 40 mm, 35 mm, 30 mm, 25 mm, 20 mm, 15 mm, 10 mm, 5 mm, or anywhere in between, upon exiting the continuous caster. In some non-limiting examples, the aluminum alloy article is cast to a gauge between about 15 mm to about 25 mm. In some cases, the aluminum alloy article is cast to a gauge of from about 15 mm to about 40 mm. Obtaining an aluminum alloy article having a similar thickness as the continuously cast aluminum article from an aluminum alloy ingot can require additional processing steps, including ingot homogenization, scalping, and breakdown rolling. In some cases, casting a thinner gauge cast aluminum alloy article (e.g., up to about 50 mm) directly from a molten alloy can significantly reduce processing time and cost. In some non-limiting examples, upon exiting a continuous casting device, the aluminum alloy article can have a caster exit temperature of from at or about 350 °C to at or about 500 °C. For example, the aluminum alloy article can have a caster exit temperature of at or about 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, or anywhere in between. - The aluminum alloy article is reheated at
block 30. In some cases, reheating atblock 30 can include solutionizing. Solutionizing can refer to a thermal treatment employed to evenly distribute alloying elements throughout an aluminum matrix within the aluminum alloy article (e.g., create a solid solution). In some examples, solutionizing a continuously cast aluminum alloy article can be performed more efficiently than solutionizing an aluminum alloy plate created from an aluminum alloy ingot. Solutionizing an aluminum alloy plate created from an aluminum alloy ingot is typically performed by heating the aluminum alloy plate created from the ingot to a solutionization temperature of about 560 °C and soaking the aluminum alloy plate at a temperature of about 560 °C for up to about 1 hour. Reheating a continuously cast aluminum alloy article as disclosed herein is performed at a peak metal temperature of from at 420 °C to at 580 °C (e.g., at 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, 570 °C, 580 °C, or anywhere in between) having a soak time of less than 5 minutes (e.g., less than 5 minutes, less than 4 minutes, less than 3 minutes, less than 2 minutes, less than 1 minute, or anywhere in between). In some non-limiting examples, reheating a continuously cast aluminum alloy article is performed at about 560 °C for less than about 3 minutes. In some aspects, decreasing the reheating temperature can require increasing the soak time, and vice versa. The aluminum alloy article can have a furnace exit temperature of from at or about 420 °C to at or about 580 °C (e.g., at or about 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, 570 °C, 580 °C, or anywhere in between). In some non-limiting examples, the furnace can be employed to maintain the caster exit temperature of the aluminum alloy article during passage from the continuous casting device to the rolling mill. - In box 40 (see
Figure 1 ), hot rolling to final gauge refers to reducing the gauge thickness of the aluminum alloy article to produce an aluminum alloy article having a desired thickness (e.g., gauge). In some cases, hot rolling to final gauge results in a thick gauge aluminum alloy article (e.g., having a thickness of 4 mm or greater such as, but not limited to, between 4 mm and about 15 mm or between about 6 mm and about 15 mm). In some cases, hot rolling a continuously cast aluminum alloy article to a final gauge can be performed more efficiently than a comparative method of breaking down an aluminum alloy ingot from a thickness of from about 450 mm to about 600 mm to a thickness of 4 mm or greater. In some examples, hot rolling a continuously cast aluminum alloy article from a gauge of from about 15 mm to about 40 mm to a final gauge of 4 mm or greater can be performed in a single pass through a hot rolling mill. In some cases, the aluminum alloy article is hot rolled to a gauge between 4 mm and about 15 mm or between about 6 mm and about 15 mm. In some cases, the percentage reduction in thickness in a single pass through the hot rolling mill can be at or about at least 35%, 40%, 45%, 50%, 55%, 60%, 65%, or 70%. In some cases, hot rolling a continuously cast aluminum alloy article from a gauge between at or about 15 mm and 40 mm to a final gauge of 4 mm or greater (such as, for example, between 4 mm and about 15 mm or between about 6 mm and about 15 mm) can be performed at a temperature of from about 400 °C to about 480 °C (e.g., at or about 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, or anywhere in between) and the aluminum alloy article can have a hot rolling mill entry temperature of from at or about 350 °C to at or about 560 °C. For example, an aluminum alloy article can have a hot rolling mill entry temperature of at or about 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, or anywhere in between. In some non-limiting examples, the aluminum alloy article can exit the furnace (e.g., solutionizing furnace) having a temperature of at or about 560 °C and have a hot rolling mill entry temperature of at or about 530 °C. In some non-limiting examples, hot rolling is performed at a temperature as hot as possible without melting the aluminum alloy article. - In some aspects, the aluminum alloy article can be subjected to hot rolling (e.g., reduction in thickness) from an as-continuously-cast gauge to a final gauge without any cold rolling. In some non-limiting examples, the aluminum alloy article can be reduced to a thick gauge aluminum article, such as 4 mm or greater, such as a aluminum alloy plate, shate, slab, sheet plate, etc. In some non-limiting examples, during hot rolling the aluminum alloy gauge can be reduced by from about 0% to about 88%. For example, the aluminum alloy article can be subjected to a reduction in gauge of 0%, 2%, 4%, 6%, 8%, 10%, 12%, 14%, 16%, 18%, 20%, 22%, 24%, 26%, 28%, 30%, 32%, 34%, 36%, 38%, 40%, 42%, 44%, 46%, 48%, 50%, 52%, 54%, 56%, 58%, 60%, 62%, 64%, 66%, 68%, 70%, 72%, 74%, 76%, 78%, 80%, 82%, 84%, 86%, 88%, or anywhere in between. In some cases, the reduction in thickness at
block 40 can be at least at or about 35%, 36%, 37%, 38%, 39%, 40%, 41%, 42%, 43%, 44%, 45%, 46%, 47%, 48%, 49%, or 50%. In some aspects, the aluminum alloy article can be hot rolled to a final gauge of 4 mm or greater, such as between 4 mm and 15 mm or between about 6 mm and about 15 mm. In some examples, the final gauge of the thick gauge aluminum alloy article is 4 mm, 5 mm, 6 mm, 7 mm, 8 mm, 9 mm, 10 mm, 11 mm, 12 mm, 13 mm, 14 mm, or 15 mm, or anywhere in between. - In some examples, the rolled aluminum alloy article can have a hot rolling mill exit temperature of from at about 380 °C to at about 450 °C. For example, the aluminum alloy article can have a hot rolling mill exit temperature of at about 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, or anywhere in between. In some non-limiting examples, the aluminum alloy article has a hot rolling mill exit temperature of at about 400 °C.
- The aluminum alloy article is thermally quenched upon exiting the rolling mill. Quenching can be performed with water and/or forced air. In some non-limiting examples, quenching is performed by spraying water onto at least a first side of the aluminum alloy article. In some cases, quenching is performed by spraying water onto a first side of the aluminum alloy article and a second side of the aluminum alloy article. In some aspects, the aluminum alloy article can be quenched by immersion in water. In some non-limiting examples, quenching can be performed at a rate of at least at or about 100 °C/second (°C/s). For example, quenching can be performed at a rate of at or about 100 °C/s, 120 °C/s, 140 °C/s, 160 °C/s, 180 °C/s, 200 °C/s, 220 °C/s, 240 °C/s, 260 °C/s, or anywhere in between. In some examples, the aluminum alloy article can be quenched to or below a temperature between at or about 200 °C and 130 °C. For example, the aluminum alloy article can be quenched to a temperature of at or about 200 °C or below, at or about 190 °C or below, at or about 180 °C or below, at or about 170 °C or below, at or about 160 °C or below, at or about 150 °C or below, at or about 140 °C or below, at or about 130 °C or below, or anywhere in between.
- Quenching is performed before rolling (e.g., to perform a lower temperature rolling, sometimes referred to as warm rolling) and after rolling. In some further cases, only minimal quenching is performed (e.g., the aluminum alloy article can be minimally quenched to a temperature of at or about 395 °C or below, at or about 390 °C or below, at or about 385 °C or below, at or about 380 °C or below, at or about 375 °C or below, at or about 370 °C or below, at or about 365 °C or below, at or about 360 °C or below, or anywhere in between, upon exiting the hot rolling mill).
- Warm rolling to final gauge can refer to reducing the gauge thickness of the aluminum alloy article at a temperature less than hot rolling to produce a thick gauge aluminum alloy article having a desired gauge (e.g., about 4 mm or greater, such as between about 4 mm and about 15 mm or between about 6 mm and about 15 mm), wherein the reduction occurs at a temperature between cold rolling and hot rolling (e.g., below a recrystallization temperature). In some cases, warm rolling a continuously cast aluminum alloy article to a final gauge can be performed to produce a thick gauge aluminum alloy article having a temper similar to any suitable temper achieved by performing cold rolling. In some examples, warm rolling a continuously cast aluminum alloy article from a gauge between at or about 15 mm and 40 mm to a final gauge of 4 mm or greater (such as, but not limited to, between 4 mm and about 15 mm or between about 6 mm and about 15 mm) can be performed in a single pass through a warm rolling mill (e.g., a hot rolling mill operating at lower temperatures). In some cases, warm rolling a continuously cast aluminum alloy article from a gauge of from at or about 15 mm to at or about 40 mm to a final gauge of from 4 mm or greater (such as, but not limited to, between 4 mm and about 15 mm or between about 6 mm and about 15 mm) can be performed at a temperature of from at or about 300 °C to at or about 400 °C (e.g., at or about 300 °C, 310 °C, 320 °C, 330 °C, 340 °C, 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, or anywhere in between) and the aluminum alloy article can have a rolling mill entry temperature for warm rolling of from at or about 350 °C to at or about 480 °C. For example, a thick gauge aluminum alloy article can have a rolling mill entry temperature of at or about 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, or anywhere in between. In some non-limiting examples, the thick gauge aluminum alloy article can exit the furnace (e.g., solutionizing furnace) at a temperature of at or about 560 °C and be subjected to quenching to a temperature of from at or about 300 °C to at or about 480 °C (e.g., at or about 300 °C, 310 °C, 320 °C, 330 °C, 340 °C, 350 °C, 360 °C, 370 °C, 380 °C, 390 °C, 400 °C, 410 °C, 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, or anywhere in between). The thick gauge aluminum alloy article can have a rolling mill entry temperature for warm rolling of less than at or about 480 °C. In some non-limiting examples, warm rolling is performed at a temperature of less than at or about 350 °C.
- In some aspects, the aluminum alloy article can be subjected to warm rolling (e.g., reduction in thickness) from an as-continuously-cast gauge to a final gauge. In some non-limiting examples, the aluminum alloy article can be reduced to a thick gauge aluminum alloy article, for example an aluminum alloy article having a thickness of 4 mm or greater (such as, but not limited to, between 4 mm and about 15 mm or between about 6 mm and about 15 mm). In some non-limiting examples, during warm rolling the aluminum alloy gauge can be reduced by from about 0% to about 88%. For example, the aluminum alloy article can be subjected to a reduction in gauge of 0%, 2%, 4%, 6%, 8%, 10%, 12%, 14%, 16%, 18%, 20%, 22%, 24%, 26%, 28%, 30%, 32%, 34%, 36%, 38%, 40%, 42%, 44%, 46%, 48%, 50%, 52%, 54%, 56%, 58%, 60%, 62%, 64%, 66%, 68%, 70%, 72%, 74%, 76%, 78%, 80%, 82%, 84%, 86%, 88%, or anywhere in between. In some cases, the reduction in thickness at
block 40 can be at least at or about 35%, 36%, 37%, 38%, 39%, 40%, 41%, 42%, 43%, 44%, 45%, 46%, 47%, 48%, 49%, or 50%. In some aspects, the aluminum alloy article can be warm rolled to a final gauge of 4 mm or greater. In some examples, the article is warm rolled to a final gauge between 4 mm and about 15 mm or between about 6 mm and about 15 mm. - Optionally, the aluminum alloy article can be reheated (e.g., solutionized) after hot or warm rolling. In some examples, reheating a hot or warm rolled continuously cast aluminum alloy article as disclosed herein can be performed at a peak metal temperature of from at or about 420 °C to at or about 580 °C (e.g., at or about 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, 570 °C, 580 °C, or anywhere in between) having a soak time of less than about 5 minutes (e.g., less than about 5 minutes, less than about 4 minutes, less than about 3 minutes, less than about 2 minutes, less than about 1 minute, or anywhere in between). In some non-limiting examples, reheating a continuously cast aluminum alloy article is performed at about 560 °C for less than about 3 minutes. In some aspects, decreasing the reheating temperature can require increasing the soak time, and vice versa. The aluminum alloy article can have a furnace exit temperature of from at or about 420 °C to at or about 580 °C (e.g., at or about 420 °C, 430 °C, 440 °C, 450 °C, 460 °C, 470 °C, 480 °C, 490 °C, 500 °C, 510 °C, 520 °C, 530 °C, 540 °C, 550 °C, 560 °C, 570 °C, 580 °C, or anywhere in between). In some cases, reheating is not performed after hot or warm rolling.
- In box 50 (see
Figure 1 ), cutting to length refers to cutting the rolled thick gauge aluminum alloy articles to a desired length (e.g., as requested by a customer) in-situ after quenching. In some non-limiting examples, aluminum alloy material is not coiled for post-production applications including storage, aging and shipping, to name a few. In some cases, after cutting, the thick gauge aluminum alloy articles (in some examples, aluminum alloy plates, shates, slabs, sheet plates or the like) can be stacked for post-production applications including storage, aging, and/or shipping, to name a few. The thick gauge aluminum alloy articles can have a stacking temperature of from at or about 100 °C or below to at or about 250 °C or below. For example, the thick gauge aluminum alloy articles can be stacked at or below a temperature of at or about 100 °C, 110 °C, 120 °C, 130 °C, 140 °C, 150 °C, 160 °C, 170 °C, 180 °C, 190 °C, 200 °C, 210 °C, 220 °C, 230 °C, 240 °C, 250 °C, or anywhere in between. - In some non-limiting examples, the stacking temperature can affect a temper of the thick gauge aluminum alloy articles. For example, stacking solutionized thick gauge aluminum alloy articles at a stacking temperature of at or about 100 °C can result in thick gauge aluminum alloy articles having a T4 temper. In some cases, stacking solutionized AA6xxx series thick gauge aluminum alloy articles at a stacking temperature of at or about 200 °C can result in AA6xxx thick gauge aluminum alloy articles having a T6 temper. In some other cases, stacking the same AA6xxx thick gauge aluminum alloy articles at a stacking temperature of at or about 250 °C can result in AA6xxx thick gauge aluminum alloy articles having a T7 temper. In some further cases, stacking solutionized AA7xxx series thick gauge aluminum alloy articles at a stacking temperature of at or about 165 °C and maintaining that temperature for at or about 24 hours can provide AA7xxx series thick gauge aluminum alloy articles having a T7 temper. Other stacking temperatures and times can be used to affect the temper of the thick gauge aluminum alloy articles as appropriate.
- In box 60 (see
Figure 1 ), artificial aging can refer to a thermal treatment process that can impart desired tempers to provided thick gauge aluminum alloy articles (in some examples, aluminum alloy plates, shates, slabs, sheet plates or the like). In some non-limiting examples, artificial aging is accomplished as part of the stacking process, such as described above. In some further examples, artificial aging is performed by further subjecting the thick gauge aluminum alloy articles to an elevated temperature suitable for artificial aging. -
Figure 2 is a schematic diagram depicting acontinuous casting system 100 according to certain aspects and features of the present disclosure. According to the invention, a pair of moving opposed casting surfaces 110 define acasting cavity 115 between the pair of moving opposed casting surfaces 110. The pair of moving opposed casting surfaces 110 can be a twin roll caster or a twin belt caster, or any other suitable continuous casting device. A molten metal injector positioned upstream of the pair of moving opposed casting surfaces 110 can inject molten metal (e.g., a molten aluminum alloy) into thecasting cavity 115 between the pair of moving opposed casting surfaces 110. The pair of moving opposed casting surfaces 110 can cast the molten aluminum alloy into a metal article, for example, analuminum alloy article 120. Casting the molten aluminum alloy into analuminum alloy article 120 can include rapidly extracting heat from the molten aluminum alloy as the molten aluminum alloy article moves through thecasting cavity 115 and thealuminum alloy article 120 exits thecasting cavity 115. Afurnace 130 positioned downstream of the pair of moving opposed casting surfaces 110 is employed to reheat thealuminum alloy article 120. Thefurnace 130 is a solutionizing furnace, which can be employed to solutionize thealuminum alloy article 120. Optionally, thefurnace 130 can be employed to maintain the cast exit temperature of thealuminum alloy article 120. In some cases, thefurnace 130 can operate at a temperature above the cast exit temperature of thealuminum alloy article 120, in which case optional heating elements positioned upstream of thefurnace 130 can increase the temperature of thealuminum alloy article 120 before it enters thefurnace 130. A rollingmill 140 positioned downstream of thefurnace 130 can be used to reduce the thickness of thealuminum alloy article 120, resulting in a thick gauge aluminum alloy article 125 (e.g., the rollingmill 140 can roll thealuminum alloy article 120 into a thick gauge aluminum alloy article 125). Aquenching device 160 positioned downstream of the rollingmill 140 is used to quench (e.g., rapidly cool) the thick gaugealuminum alloy article 125. Aplate shearing device 170 positioned downstream of thequenching device 160 can be employed to cut the thick gaugealuminum alloy article 125 to a desired length. If desired, the cut thick gaugealuminum alloy article 125 is then stacked into astack 180 of thick gaugealuminum alloy articles 125 for any suitable further downstream processing. - A
second quenching device 165 is positioned upstream of the rollingmill 140 to quench thealuminum alloy article 120 prior to rolling. In some cases, such asecond quenching device 165 can be suitable for use with a warm rolling procedure (e.g., rolling at temperatures below the recrystallization temperature). The use of asecond quenching device 165 immediately before rolling can result in the thick gaugealuminum alloy article 125 having mechanical properties similar to aluminum alloy rolled articles having a T3 or a T8 temper (e.g., high strength, and precipitation hardened). For example, the methods described above can provide thick gauge aluminum alloy articles (e.g., plates, shates, slabs, sheet plates, etc.) having mechanical properties similar to aluminum alloy articles produced via cold working (e.g., cold rolling) even though the thick gauge aluminum alloy articles described herein are not cold rolled. In some aspects, mechanical properties exhibited by aluminum alloys having a T3 or a T8 temper as described above can be imparted to the thick gauge aluminum alloy articles described herein using the methods described herein. For example, where T8 temper properties are desired, an aluminum alloy can be subjected to continuous casting, solutionizing, quenching, hot rolling to a final gauge and quenching after hot rolling, described in detail below. - In some non-limiting examples, the
continuous casting system 100 can be arranged in a plurality of configurations to provide a specifically-tailored thermal history for the thick gaugealuminum alloy articles 125. Described herein is that an AA6xxx series aluminum alloy in T4, T6, or T7 temper can be produced by casting an aluminum alloy article 120 such that the aluminum alloy article 120 exiting the casting cavity 115 has a caster exit temperature of about 450 °C, solutionizing in the solutionizing furnace 130 at a temperature of about 560 °C, and subjecting the aluminum alloy article 120 to a 50% reduction in the rolling mill 140 at a temperature between approximately 530 °C and 580 °C. For T4 temper, the thick gauge aluminum alloy article 125 can exit the rolling mill 140 and be immediately quenched using a quenching device 160 to a temperature at or below 200 °C, then cut using cutting device 160 and stacked at a temperature at or below 100 °C. For T6 temper, the thick gauge aluminum alloy article 125 can exit the rolling mill 140 and be immediately quenched using a quenching device 160 to a temperature at or about 200 °C, then cut using cutting device 160 and stacked at a temperature at or about 200 °C. For T7 temper, the thick gauge aluminum alloy article 125 can exit the rolling mill 140 and be immediately quenched using a quenching device 160 to a temperature at or about 250 °C, then cut using cutting device 160 and stacked at a temperature at or about 250 °C. - In an example, an AA6xxx series aluminum alloy having T3 or T8 temper properties (e.g., high strength) can be produced without cold rolling. The AA6xxx series aluminum alloy having T3 or T8 temper properties can be provided by casting an aluminum alloy article 120 such that the aluminum alloy article 120 exiting the casting cavity 115 has a caster exit temperature of about 450 °C, solutionizing in the solutionizing furnace 130 at a temperature of about 560 °C, then quenching the aluminum alloy article 120 using quenching device 165 to a temperature of about 470 °C before subjecting the aluminum alloy article 120 to a 50% reduction in the rolling mill 140 at a temperature below approximately 500 °C, such as at or about 470 °C. The resultant thick gauge aluminum alloy article 125 can exit the rolling mill 140 at a rolling mill exit temperature of about 400 °C and be immediately quenched using quenching device 160 to a temperature of at or below about 200 °C. To provide the AA6xxx series aluminum alloy having T3 temper properties, the thick gauge aluminum alloy article 125 can be cut using cutting device 160 and stacked at a temperature at or below 100 °C. To provide the AA6xxx series aluminum alloy having T8 temper properties, the thick gauge aluminum alloy article 125 can be cut using cutting device 160 and stacked at a temperature at or about 200 °C. To provide the AA6xxx series aluminum alloy having T8x temper properties, the thick gauge aluminum alloy article 125 can be cut using cutting device 160, stacked at a temperature at or about 200 °C, and artificially aged.
- The following examples will serve to further illustrate the present invention without, at the same time, however, constituting any limitation thereof. On the contrary, it is to be clearly understood that resort may be had to various embodiments, modifications and equivalents thereof which, after reading the description herein, may suggest themselves to those skilled in the art without departing from the spirit of the invention. During the studies described in the following examples, conventional procedures were followed, unless otherwise stated. Some of the procedures are described below for illustrative purposes.
- Various alloys were prepared for strength, elongation, and formability testing. The chemical compositions for these alloys are provided in Table 1 below.
Table 1: Alloy Compositions Element Alloy A Alloy B Si 0.70 0.80 Fe 0.20 0.20 Cu 0.85 0.80 Mn 0.30 0.18 Mg 0.90 0.80 Ti 0.04 0.02 Cr 0.03 0.07 Zr 0.12 0.00 Impurities 0.05 (each) 0.05 (each) 0.15 (total) 0.15 (total) A1 Remainder Remainder - All values expressed as weight percentage (wt. %) of the whole.
- Alloy A and Alloy B (see Table 1) were provided in a T4 temper, a partial T6 temper, and a full T6 temper by employing the methods described above and optional artificial aging. For example, Alloy A and Alloy B can be produced by the methods depicted in
Figure 1 , including casting an aluminum alloy article such that the aluminum alloy article exiting thecasting cavity 115 has a caster exit temperature of about 450 °C, solutionizing in thesolutionizing furnace 130 at a temperature of from about 550 °C to about 570 °C for 2 minutes, and subjecting thealuminum alloy article 120 to about a 40% to about a 70% reduction in the rollingmill 140 at a temperature between approximately 530 °C and 580 °C. Alloy A was reduced about 40% to a gauge of 9.5 mm. Alloy B was reduced about 70% to a gauge of 5.0 mm. For T4 temper, a thick gauge aluminum alloy article can exit the rollingmill 140 and be immediately quenched using thequenching device 160 to a temperature at or below 50 °C, then cut using thecutting device 160 and stacked at a temperature at or below 100 °C. For partial T6 temper, the thick gauge aluminum alloy articles can be artificially aged at 200 °C for 2 hours. For full T6 temper, the thick gauge aluminum alloy articles can be artificially aged at 180 °C for 10 hours. -
Figure 3 is a chart depicting mechanical properties of thick gauge aluminum alloy articles made from Alloy A and Alloy B. Both Alloy A and Alloy B exhibited high strength after artificial aging (e.g., in partial T6 temper and full T6 temper) having yield strength (referred to as "YS" inFigure 3 ) (left histogram in each group) of from about 330 MPa to about 345 MPa. Both Alloy A and Alloy B exhibited ample strength after natural aging (e.g., in T4 temper) having yield strength (left histogram in each group) of from about 180 MPa to about 200 MPa, and excellent deformability (e.g., uniform elongation, referred to as "UE" inFigure 3 and represented by open circles) of about 21% to about 22% UE. In some aspects, having a UE of about 21% to about 22% can allow a 90° bend during forming (e.g., stamping, or bending) without fracture or failure. Additionally, Alloy A and Alloy B exhibited high ultimate tensile strengths (referred to as "UTS" inFigure 3 ) (right histogram in each group), as well as high total elongation before fracture (referred to as "TE" inFigure 3 and represented by open diamonds). - The foregoing description of the embodiments, including illustrated embodiments, has been presented only for the purpose of illustration and description and is not intended to be exhaustive or limiting to the precise forms disclosed. Numerous modifications, adaptations, and uses thereof will be apparent to those skilled in the art.
Claims (10)
- A method for producing rolled aluminum alloy articles, comprising:providing a molten aluminum alloy;continuously casting (20) an aluminum alloy article (120) from the molten aluminum alloy;rolling (40) the aluminum alloy article (120) at a rolling temperature from 300 °C to 580 °C to a gauge of 4 millimeters (mm) or greater to produce a rolled aluminum alloy article (125),reheating (30) the aluminum alloy article (120) after continuous casting (20) and before rolling (40),quenching the aluminum alloy article (120) immediately before rolling (40), andquenching the aluminum alloy article (120) after rolling,wherein the reheating (30) the aluminum alloy article (120) comprises reheating the aluminum alloy article (120) to a peak metal temperature from 420 °C to 580 °C and maintaining the peak metal temperature for a duration of between 1 minute to 5 minutes.
- The method of claim 1, wherein the molten aluminum alloy is an AA7xxx series aluminum alloy, and wherein the reheating (30) the aluminum alloy article (120) comprises reheating the aluminum alloy article (120) to a peak metal temperature of at 480 °C or, wherein the molten aluminum alloy is an AA6xxx series aluminum alloy, and wherein the reheating (30) the aluminum alloy article (120) comprises reheating the aluminum alloy article (120) to a peak metal temperature of at 560 °C.
- The method of claim 1, further comprising quenching the rolled aluminum alloy article (125) at a rate of at least 100 °C/second after rolling (40).
- The method of claim 1, further comprising cutting (50) the rolled aluminum alloy article (125) after rolling (40) to produce cut and rolled aluminum alloy articles.
- The method of claim 4, further comprising stacking the cut and rolled aluminum alloy articles after cutting (50).
- The method of claim 5, wherein stacking the cut and rolled aluminum alloy articles after cutting (50) is performed at a cut and rolled aluminum alloy article temperature of from 100 °C to 250 °C and
in particular, wherein stacking the cut and rolled aluminum alloy articles provides a desired temper. - The method of claim 1, further comprising artificially aging (60) the rolled aluminum alloy article (125).
- The method of claim 1, wherein a continuous casting exit temperature of the aluminum alloy article (120) is from 350 °C to 500 °C.
- The method of claim 1, wherein rolling (40) the aluminum alloy article (120) comprises warm rolling the aluminum alloy article (120) at a warm rolling temperature of from 300 °C to 400 °C.
- A continuous casting system, suitable for carrying the method of any of claims 1-9, comprising:a pair of moving opposed casting surfaces (110) spaced apart to define a casting cavity (115) therebetween, wherein the casting cavity (115) is sized to cast the aluminum alloy article (120) at a first thickness;a solutionizing furnace (130) positioned downstream of the pair of moving opposed casting surfaces (110);a rolling mill (140) positioned downstream of the solutionizing furnace (130), wherein the rolling mill (140) is configured to reduce the aluminum alloy article (120) from the first thickness to a thickness of at least 4 mm;at least a first quenching device (160) positioned downstream of the rolling mill (140);at least a second quenching device (165) positioned upstream of the rolling mill (140);a cutting device (170) positioned downstream of at least the first quenching device (160); anda stacking device positioned downstream of the cutting device.
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PCT/US2017/053720 WO2018080706A1 (en) | 2016-10-27 | 2017-09-27 | Systems and methods for making thick gauge aluminum alloy articles |
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Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU2016369546B2 (en) | 2015-12-18 | 2019-06-13 | Novelis Inc. | High strength 6xxx aluminum alloys and methods of making the same |
EP3532213B1 (en) | 2016-10-27 | 2021-09-01 | Novelis, Inc. | Apparatus and method for making thick gauge aluminum alloy articles |
EP3532219B1 (en) | 2016-10-27 | 2023-05-31 | Novelis, Inc. | High strength 6xxx series aluminum alloys and methods of making the same |
CN109890536B (en) | 2016-10-27 | 2022-09-23 | 诺维尔里斯公司 | High strength7XXX series aluminum alloys and methods of making the same |
CN112119176A (en) * | 2018-05-15 | 2020-12-22 | 诺维尔里斯公司 | High strength 6XXX and 7XXX aluminum alloys and methods of making the same |
KR20230042406A (en) | 2018-05-15 | 2023-03-28 | 노벨리스 인크. | F* and w temper aluminum alloy products and methods of making the same |
WO2020123807A1 (en) * | 2018-12-12 | 2020-06-18 | Peter Von Czarnowski | Method and system for heat treatment of metal alloy sheet |
ES2929001T3 (en) * | 2019-12-23 | 2022-11-24 | Novelis Koblenz Gmbh | Manufacturing process of an aluminum alloy rolled product |
CN111077178B (en) * | 2020-01-16 | 2021-09-24 | 昆明理工大学 | High-flux spray quenching sample clamping device |
FI20205279A1 (en) * | 2020-03-19 | 2021-09-20 | Upcast Oy | Process of producing a non-ferrous metallic tube |
JP2023519380A (en) * | 2020-04-03 | 2023-05-10 | ノベリス・インコーポレイテッド | High temperature decoiling of metal |
EP3974072B1 (en) * | 2020-09-24 | 2023-07-19 | Primetals Technologies Austria GmbH | Casting roller composite system and method for operating the casting roller composite system |
WO2022192812A1 (en) | 2021-03-12 | 2022-09-15 | Novelis Inc. | High-strength 5xxx aluminum alloy variants and methods for preparing the same |
CN113745631B (en) * | 2021-08-31 | 2022-11-11 | 湖北亿纬动力有限公司 | Battery roll core flattening method |
CN115254955A (en) * | 2022-05-06 | 2022-11-01 | 湖南工业大学 | Rolling method of aluminum alloy sheet |
TWI799335B (en) * | 2022-08-15 | 2023-04-11 | 中國鋼鐵股份有限公司 | Hot rolled steel and manufacturing method the same |
Family Cites Families (123)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3612151A (en) | 1969-02-14 | 1971-10-12 | Kaiser Aluminium Chem Corp | Control of continuous casting |
GB1387992A (en) | 1971-02-16 | 1975-03-19 | Alcan Res & Dev | Apparatus for continuous casting |
US3933193A (en) | 1971-02-16 | 1976-01-20 | Alcan Research And Development Limited | Apparatus for continuous casting of metal strip between moving belts |
US4028141A (en) | 1975-03-12 | 1977-06-07 | Southwire Company | Aluminum iron silicon alloy |
CH624147A5 (en) | 1976-12-24 | 1981-07-15 | Alusuisse | |
US4194553A (en) * | 1978-06-05 | 1980-03-25 | Hitachi, Ltd. | Cooling and guide method and apparatus in a continuous casting machine |
US4235646A (en) | 1978-08-04 | 1980-11-25 | Swiss Aluminium Ltd. | Continuous strip casting of aluminum alloy from scrap aluminum for container components |
US4238248A (en) | 1978-08-04 | 1980-12-09 | Swiss Aluminium Ltd. | Process for preparing low earing aluminum alloy strip on strip casting machine |
FR2526047A1 (en) | 1982-04-30 | 1983-11-04 | Conditionnements Aluminium | PROCESS FOR THE PRODUCTION OF ALUMINUM ALLOY PRODUCTS FOR STRETCHING |
DE3241745C2 (en) | 1982-11-11 | 1985-08-08 | Mannesmann AG, 4000 Düsseldorf | Process for the production of hot-rolled steel strip from continuously cast raw material in directly successive work steps |
US4753685A (en) | 1983-02-25 | 1988-06-28 | Kabushiki Kaisha Kobe Seiko Sho | Aluminum alloy sheet with good forming workability and method for manufacturing same |
US4614552A (en) | 1983-10-06 | 1986-09-30 | Alcan International Limited | Aluminum alloy sheet product |
JPS60152348A (en) | 1984-01-18 | 1985-08-10 | Mitsubishi Heavy Ind Ltd | Belt type continuous casting machine |
JPS621839A (en) | 1985-06-26 | 1987-01-07 | Sky Alum Co Ltd | Wear resistant rolled aluminum alloy plate |
JPS6283453A (en) | 1985-10-07 | 1987-04-16 | Sumitomo Alum Smelt Co Ltd | Manufacture of aluminum alloy ingot for extrusion |
JPS6289502A (en) | 1985-10-12 | 1987-04-24 | Sumitomo Metal Ind Ltd | Production of steel sheet by continuous casting of thin ingot |
DE3760023D1 (en) | 1986-02-13 | 1989-01-26 | Larex Ag | Method and apparatus for continuous twin-roll casting |
US4808247A (en) | 1986-02-21 | 1989-02-28 | Sky Aluminium Co., Ltd. | Production process for aluminum-alloy rolled sheet |
JPH0636965B2 (en) * | 1987-01-27 | 1994-05-18 | 三菱重工業株式会社 | Belt type continuous casting machine |
JPS63252604A (en) | 1987-04-08 | 1988-10-19 | Hitachi Ltd | Method and apparatus for rolling coupled directly to continuous casting |
US5244516A (en) | 1988-10-18 | 1993-09-14 | Kabushiki Kaisha Kobe Seiko Sho | Aluminum alloy plate for discs with improved platability and process for producing the same |
US5046347A (en) | 1989-10-10 | 1991-09-10 | Alcan International Limited | Coolant containment apparatus for rolling mills |
DE4121489C2 (en) | 1991-06-26 | 1994-08-04 | Mannesmann Ag | Furnace plant as a buffer behind a thin slab caster |
JPH0819509B2 (en) | 1991-07-31 | 1996-02-28 | リョービ株式会社 | Method for producing high strength aluminum alloy |
GB9221438D0 (en) * | 1992-10-13 | 1992-11-25 | Philips Electronics Nv | Time management for cordless telephone |
TW245661B (en) * | 1993-01-29 | 1995-04-21 | Hitachi Seisakusyo Kk | |
US5616189A (en) | 1993-07-28 | 1997-04-01 | Alcan International Limited | Aluminum alloys and process for making aluminum alloy sheet |
JPH0790459A (en) | 1993-09-17 | 1995-04-04 | Mitsubishi Alum Co Ltd | Production of wear resistant aluminum alloy for extrusion and wear resistant aluminum alloy material |
FR2716896B1 (en) | 1994-03-02 | 1996-04-26 | Pechiney Recherche | Alloy 7000 with high mechanical resistance and process for obtaining it. |
JPH07252573A (en) | 1994-03-17 | 1995-10-03 | Kobe Steel Ltd | Al-zn-mg-cu alloy excellent in toughness and its production |
DE69507398T2 (en) | 1994-08-05 | 1999-05-27 | Fuji Photo Film Co., Ltd., Minami-Ashigara, Kanagawa | Aluminum alloy carrier for a high pressure plate and method of manufacturing the same |
BR9611416A (en) * | 1995-09-18 | 1999-02-23 | Kaiser Aluminium Chem Corp | Processes for the manufacture of tabs and can tops for aluminum alloy containers of tab material and can tops for aluminum alloy containers and aluminum alloy sheet material lid or tin tab for aluminum alloy containers and material for lid or can tab for aluminum alloy containers |
AUPN733095A0 (en) | 1995-12-22 | 1996-01-25 | Bhp Steel (Jla) Pty Limited | Twin roll continuous caster |
JPH09327706A (en) | 1996-06-07 | 1997-12-22 | Ishikawajima Harima Heavy Ind Co Ltd | Hot continuous rolling equipment |
US5850020A (en) * | 1996-09-11 | 1998-12-15 | Genesis Research & Development Corporation, Ltd. | Materials and method for the modification of plant lignin content |
JPH10130768A (en) | 1996-10-30 | 1998-05-19 | Furukawa Electric Co Ltd:The | Directly cast and rolled sheet of al-mg-si alloy for forming, and its production |
EP0970259B1 (en) | 1997-03-07 | 2002-10-16 | Alcan International Limited | Process for producing aluminium sheet |
FR2763602B1 (en) | 1997-05-20 | 1999-07-09 | Pechiney Rhenalu | METHOD OF MANUFACTURING STRIPS OF ALUMINUM ALLOYS BY THIN CONTINUOUS CASTING BETWEEN CYLINDERS |
WO1998055663A1 (en) | 1997-06-04 | 1998-12-10 | Golden Aluminum Company | Continuous casting process for producing aluminum alloys having low earing |
DE19725434C2 (en) * | 1997-06-16 | 1999-08-19 | Schloemann Siemag Ag | Process for rolling hot wide strip in a CSP plant |
US20030173003A1 (en) | 1997-07-11 | 2003-09-18 | Golden Aluminum Company | Continuous casting process for producing aluminum alloys having low earing |
JP2000017412A (en) | 1998-07-01 | 2000-01-18 | Furukawa Electric Co Ltd:The | Production of aluminum alloy sheet |
JP4229307B2 (en) | 1998-11-20 | 2009-02-25 | 住友軽金属工業株式会社 | Aluminum alloy plate for aircraft stringers having excellent stress corrosion cracking resistance and method for producing the same |
US6537398B1 (en) | 1998-12-18 | 2003-03-25 | Avestapolarit Ab (Publ) | Method for manufacturing of strips of stainless steel and integrated rolling mill line |
JP3495278B2 (en) | 1999-01-26 | 2004-02-09 | 株式会社神戸製鋼所 | Belt type continuous casting apparatus and belt type continuous casting method |
US6289972B1 (en) | 1999-05-21 | 2001-09-18 | Danieli Technology Inc. | Integrated plant for the production of rolled stock |
CA2392617A1 (en) * | 1999-12-17 | 2001-06-21 | Helene P. Lagace | Method of quenching alloy sheet to minimize distortion |
US6755236B1 (en) | 2000-08-07 | 2004-06-29 | Alcan International Limited | Belt-cooling and guiding means for continuous belt casting of metal strip |
GB2366531B (en) | 2000-09-11 | 2004-08-11 | Daido Metal Co | Method and apparatus for continuous casting of aluminum bearing alloy |
DE10116636C2 (en) | 2001-04-04 | 2003-04-03 | Vaw Ver Aluminium Werke Ag | Process for the production of AIMn strips or sheets |
NL1018817C2 (en) | 2001-08-24 | 2003-02-25 | Corus Technology B V | Method for processing a continuously cast metal slab or belt, and plate or belt thus produced. |
FR2835533B1 (en) | 2002-02-05 | 2004-10-08 | Pechiney Rhenalu | AL-Si-Mg ALLOY SHEET FOR AUTOMOTIVE BODY SKIN |
US20040011438A1 (en) | 2002-02-08 | 2004-01-22 | Lorentzen Leland L. | Method and apparatus for producing a solution heat treated sheet |
US6789602B2 (en) * | 2002-02-11 | 2004-09-14 | Commonwealth Industries, Inc. | Process for producing aluminum sheet product having controlled recrystallization |
CA2485525C (en) | 2002-06-24 | 2010-09-21 | Corus Aluminium Walzprodukte Gmbh | Method of producing high strength balanced al-mg-si alloy and a weldable product of that alloy |
US6811625B2 (en) | 2002-10-17 | 2004-11-02 | General Motors Corporation | Method for processing of continuously cast aluminum sheet |
US7048815B2 (en) | 2002-11-08 | 2006-05-23 | Ues, Inc. | Method of making a high strength aluminum alloy composition |
US6764559B2 (en) | 2002-11-15 | 2004-07-20 | Commonwealth Industries, Inc. | Aluminum automotive frame members |
EP1697069B1 (en) | 2003-10-03 | 2009-07-15 | Novelis Inc. | Belt casting of non-ferrous and light metals and apparatus therefor |
WO2005032743A1 (en) | 2003-10-03 | 2005-04-14 | Novelis Inc. | Surface texturing of casting belts of continuous casting machines |
US6959476B2 (en) | 2003-10-27 | 2005-11-01 | Commonwealth Industries, Inc. | Aluminum automotive drive shaft |
TW200536946A (en) | 2003-12-11 | 2005-11-16 | Nippon Light Metal Co | Method for producing Al-Mg-Si alloy excellent in bake-hardenability and hemmability |
US7182825B2 (en) | 2004-02-19 | 2007-02-27 | Alcoa Inc. | In-line method of making heat-treated and annealed aluminum alloy sheet |
US20050211350A1 (en) * | 2004-02-19 | 2005-09-29 | Ali Unal | In-line method of making T or O temper aluminum alloy sheets |
JP4222964B2 (en) * | 2004-04-09 | 2009-02-12 | トヨタ自動車株式会社 | Aluminum alloy plate for automobile outer plate, method for producing the same and automobile outer plate |
PT1868748E (en) | 2005-04-07 | 2008-12-12 | Giovanni Arvedi | Process and system for manufacturing metal strips and sheets without solution of continuity between continuous casting and rolling |
CN100532603C (en) | 2005-05-25 | 2009-08-26 | 日本轻金属株式会社 | Aluminum alloy thin plate and its making method |
JP2007031819A (en) * | 2005-07-29 | 2007-02-08 | Nippon Light Metal Co Ltd | Method for producing aluminum alloy sheet |
DE102006054932A1 (en) | 2005-12-16 | 2007-09-13 | Sms Demag Ag | Method and device for producing a metal strip by casting rolls |
RU2299256C1 (en) | 2005-12-27 | 2007-05-20 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") | Aluminum-based alloy and article made therefrom |
JP4203508B2 (en) | 2006-03-08 | 2009-01-07 | 株式会社神戸製鋼所 | Method for producing aluminum alloy cast plate |
RU2305022C1 (en) | 2006-03-13 | 2007-08-27 | Государственное образовательное учреждение высшего профессионального образования "Уральский государственный технический университет-УПИ" | Method for producing foil blank of aluminum-iron-silicon alloy |
JP4939093B2 (en) | 2006-03-28 | 2012-05-23 | 株式会社神戸製鋼所 | Method for producing 6000 series aluminum alloy plate for automobile panel having excellent hem bendability and bake hardness |
RU2313594C1 (en) | 2006-04-03 | 2007-12-27 | Открытое Акционерное Общество "Корпорация Всмпо-Ависма" | Aluminum-based alloy |
DE102007022931A1 (en) * | 2006-05-26 | 2007-11-29 | Sms Demag Ag | Production of a metal strip used in a continuous casting process comprises using rolling and milling operations directly with casting of a slab in a casting machine |
FR2907466B1 (en) | 2006-07-07 | 2011-06-10 | Aleris Aluminum Koblenz Gmbh | ALUMINUM ALLOY PRODUCTS OF THE AA7000 SERIES AND METHOD FOR MANUFACTURING THE SAME |
EP2048259A4 (en) | 2006-08-01 | 2015-03-18 | Showa Denko Kk | Process for production of aluminum alloy formings, aluminum alloy formings and production system |
JP4690279B2 (en) | 2006-09-22 | 2011-06-01 | 株式会社神戸製鋼所 | Evaluation method of stress corrosion cracking resistance of aluminum alloy materials |
JP2008190022A (en) | 2007-02-07 | 2008-08-21 | Kobe Steel Ltd | Al-Mg-Si-BASED ALLOY HOT ROLLED SHEET, AND METHOD FOR PRODUCING THE SAME |
DE112008003052T5 (en) | 2007-11-15 | 2010-12-16 | Aleris Aluminum Koblenz Gmbh | Product of Al-Mg-Zn wrought alloy and manufacturing method therefor |
DE112009000981T5 (en) | 2008-04-25 | 2011-03-24 | Aleris Aluminium Duffel Bvba | Method for producing an aluminum alloy component |
JP2009293071A (en) * | 2008-06-04 | 2009-12-17 | Mazda Motor Corp | Continuously cast and rolled material and method for producing plastic-worked member using the continuously cast and rolled material |
US20110111081A1 (en) * | 2008-06-24 | 2011-05-12 | Aleris Aluminum Koblenz Gmbh | Al-zn-mg alloy product with reduced quench sensitivity |
WO2010066412A1 (en) | 2008-12-09 | 2010-06-17 | Sms Siemag Ag | Method for producing strips of metal, and production line for performing the method |
US8459333B2 (en) * | 2009-05-06 | 2013-06-11 | Siemens Aktiengesellschaft | Method for producing rolling stock rolled in a rolling train of a rolling mill, control and/or regulation device for rolling mill for producing rolled rolling stock, rolling mill for producing rolled rolling stock, machine readable program code and storage medium |
RU2415193C1 (en) | 2009-12-24 | 2011-03-27 | Открытое Акционерное Общество "МОСОБЛПРОММОНТАЖ" | Cast alloy on base of aluminium |
WO2012033939A2 (en) | 2010-09-08 | 2012-03-15 | Alcoa Inc. | Improved 7xxx aluminum alloys, and methods for producing the same |
RU102550U1 (en) | 2010-10-13 | 2011-03-10 | Федеральное Государственное Автономное Образовательное Учреждение Высшего Профессионального Образования "Сибирский Федеральный Университет" | INSTALLATION FOR CONTINUOUS CASTING, ROLLING AND PRESSING OF METAL |
PL2554281T3 (en) * | 2011-08-01 | 2017-08-31 | Primetals Technologies Germany Gmbh | Method and apparatus for a continuous rolling |
EP2813592B1 (en) | 2012-02-10 | 2016-09-21 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | Aluminum alloy sheet for connecting components and manufacturing process therefor |
AU2013202557B2 (en) | 2012-03-07 | 2017-06-15 | Arconic Inc. | Improved 6XXX aluminum alloys and methods for producing the same |
WO2013133960A1 (en) * | 2012-03-07 | 2013-09-12 | Alcoa Inc. | Improved 7xxx aluminum alloys, and methods for producing the same |
US9856552B2 (en) * | 2012-06-15 | 2018-01-02 | Arconic Inc. | Aluminum alloys and methods for producing the same |
US20150275339A1 (en) | 2012-06-28 | 2015-10-01 | Jfe Steel Corporation | High-carbon steel tube having superior cold workability, machinability, and hardenability and method for manufacturing the same |
JP5854954B2 (en) | 2012-08-30 | 2016-02-09 | 株式会社デンソー | High-strength aluminum alloy fin material and manufacturing method thereof |
DE102012215599A1 (en) | 2012-09-03 | 2014-03-06 | Sms Siemag Ag | Method and device for the dynamic supply of a cooling device for cooling metal strip or other rolling stock with coolant |
CN104619872A (en) | 2012-09-20 | 2015-05-13 | 株式会社神户制钢所 | Aluminum alloy automobile part |
US9587298B2 (en) | 2013-02-19 | 2017-03-07 | Arconic Inc. | Heat treatable aluminum alloys having magnesium and zinc and methods for producing the same |
CN103131904B (en) | 2013-03-06 | 2015-03-25 | 佛山市三水凤铝铝业有限公司 | Aluminum alloy material and heat treatment technique thereof |
ES2649160T3 (en) | 2013-03-11 | 2018-01-10 | Novelis, Inc. | Improved flatness of a laminated tape |
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